FR3109142B1 - Removable shutter member for a female part housed in an external opening of an aircraft nacelle - Google Patents

Removable shutter member for a female part housed in an external opening of an aircraft nacelle Download PDF

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Publication number
FR3109142B1
FR3109142B1 FR2003633A FR2003633A FR3109142B1 FR 3109142 B1 FR3109142 B1 FR 3109142B1 FR 2003633 A FR2003633 A FR 2003633A FR 2003633 A FR2003633 A FR 2003633A FR 3109142 B1 FR3109142 B1 FR 3109142B1
Authority
FR
France
Prior art keywords
female part
shutter member
nacelle
external opening
removable shutter
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
FR2003633A
Other languages
French (fr)
Other versions
FR3109142A1 (en
Inventor
Olivier Meriel
Vivien Lucienne
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Nacelles SAS
Original Assignee
Safran Nacelles SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Safran Nacelles SAS filed Critical Safran Nacelles SAS
Priority to FR2003633A priority Critical patent/FR3109142B1/en
Priority to PCT/FR2021/050626 priority patent/WO2021205126A1/en
Priority to US17/995,508 priority patent/US20230174245A1/en
Priority to EP21723889.8A priority patent/EP4132848B1/en
Priority to CN202180027587.3A priority patent/CN115397734A/en
Publication of FR3109142A1 publication Critical patent/FR3109142A1/en
Application granted granted Critical
Publication of FR3109142B1 publication Critical patent/FR3109142B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00—Power-plant nacelles, fairings, or cowlings
    • B64D29/08—Inspection panels for power plants
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/08—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of power plant cooling systems
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/40—Maintaining or repairing aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/50—Handling or transporting aircraft components
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/60—Fluid transfer
    • F05D2260/607—Preventing clogging or obstruction of flow paths by dirt, dust, or foreign particles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/50—Intrinsic material properties or characteristics
    • F05D2300/501—Elasticity
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Transportation (AREA)
  • Manufacturing & Machinery (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Wind Motors (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Connection Of Plates (AREA)
  • Pressure Vessels And Lids Thereof (AREA)

Abstract

Organe d’obturation (50) amovible configuré pour obturer une partie femelle (40) logée dans une ouverture extérieure (16b) pratiquée dans la surface extérieure (16) d’une nacelle (10) pour moteur d’aéronef, ladite partie femelle (40) comprenant au moins un orifice d’entrée d’air (48). Ledit organe d’obturation (50) comprend une embase (51) formant le contour extérieur dudit organe et s’étendant au-delà de l’ouverture extérieure (16b) de la nacelle (10) de manière à venir en appui sur la surface extérieure (16) de ladite nacelle et au moins un organe de maintien en position (56) élastiquement déformable en saillie depuis l’embase (51) et configuré pour s’insérer dans l’orifice d’entrée d’air (48). Figure pour l’abrégé : Fig 9Removable shutter member (50) configured to shut off a female part (40) housed in an outer opening (16b) made in the outer surface (16) of a nacelle (10) for an aircraft engine, said female part ( 40) comprising at least one air inlet (48). Said closure member (50) comprises a base (51) forming the outer contour of said member and extending beyond the outer opening (16b) of the nacelle (10) so as to bear against the surface exterior (16) of said nacelle and at least one elastically deformable position-holding member (56) projecting from the base (51) and configured to be inserted into the air inlet orifice (48). Figure for abstract: Fig 9

FR2003633A 2020-04-10 2020-04-10 Removable shutter member for a female part housed in an external opening of an aircraft nacelle Active FR3109142B1 (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR2003633A FR3109142B1 (en) 2020-04-10 2020-04-10 Removable shutter member for a female part housed in an external opening of an aircraft nacelle
PCT/FR2021/050626 WO2021205126A1 (en) 2020-04-10 2021-04-08 Removable closure member for a female portion received in an external opening of an aircraft engine nacelle
US17/995,508 US20230174245A1 (en) 2020-04-10 2021-04-08 Removable closure member for a female portion received in an external opening of an aircraft engine nacelle
EP21723889.8A EP4132848B1 (en) 2020-04-10 2021-04-08 Removable closure body for a female part housed in an exterior opening of an aircraft engine nacelle
CN202180027587.3A CN115397734A (en) 2020-04-10 2021-04-08 Removable closing member for a female portion received in an external opening of an aircraft engine nacelle

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2003633A FR3109142B1 (en) 2020-04-10 2020-04-10 Removable shutter member for a female part housed in an external opening of an aircraft nacelle
FR2003633 2020-04-10

Publications (2)

Publication Number Publication Date
FR3109142A1 FR3109142A1 (en) 2021-10-15
FR3109142B1 true FR3109142B1 (en) 2022-03-04

Family

ID=71094544

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2003633A Active FR3109142B1 (en) 2020-04-10 2020-04-10 Removable shutter member for a female part housed in an external opening of an aircraft nacelle

Country Status (5)

Country Link
US (1) US20230174245A1 (en)
EP (1) EP4132848B1 (en)
CN (1) CN115397734A (en)
FR (1) FR3109142B1 (en)
WO (1) WO2021205126A1 (en)

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2879564B1 (en) * 2004-12-20 2008-05-16 Airbus France Sas VENTILATION AIR ENTRY ARRANGEMENT WITH MOBILE SHUTTER ELEMENT
FR2936778B1 (en) * 2008-10-07 2011-06-10 Airbus France AIR INTAKE ARRANGEMENT FOR AIRCRAFT
FR3010701B1 (en) * 2013-09-13 2015-10-09 Snecma ARRANGEMENT OF A TANK BETWEEN A NACELLE HOOD AND A TURBOMACHINE
US9972896B2 (en) * 2016-06-23 2018-05-15 General Electric Company Wireless aircraft engine monitoring system
US10640223B2 (en) * 2017-08-22 2020-05-05 Rohr, Inc. Safety maintenance panel for a thrust reverser

Also Published As

Publication number Publication date
WO2021205126A1 (en) 2021-10-14
EP4132848B1 (en) 2024-01-31
US20230174245A1 (en) 2023-06-08
EP4132848A1 (en) 2023-02-15
CN115397734A (en) 2022-11-25
FR3109142A1 (en) 2021-10-15

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